BRPI0908328A2 - propulsion inverters, control device and aircraft application process - Google Patents

propulsion inverters, control device and aircraft application process

Info

Publication number
BRPI0908328A2
BRPI0908328A2 BRPI0908328A BRPI0908328A BRPI0908328A2 BR PI0908328 A2 BRPI0908328 A2 BR PI0908328A2 BR PI0908328 A BRPI0908328 A BR PI0908328A BR PI0908328 A BRPI0908328 A BR PI0908328A BR PI0908328 A2 BRPI0908328 A2 BR PI0908328A2
Authority
BR
Brazil
Prior art keywords
control device
application process
aircraft application
inverters
propulsion
Prior art date
Application number
BRPI0908328A
Other languages
Portuguese (pt)
Inventor
Phillipe Abrial
Phillipe Feiullard
Original Assignee
Airbus Operations Sas
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI0908328A2 publication Critical patent/BRPI0908328A2/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Retarders (AREA)
  • Control Of Transmission Device (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Turbines (AREA)
BRPI0908328A 2008-05-06 2009-04-30 propulsion inverters, control device and aircraft application process BRPI0908328A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0802511A FR2930973B1 (en) 2008-05-06 2008-05-06 METHOD AND DEVICE FOR IMPLEMENTING THE THRUST INVERTERS OF AN AIRCRAFT
PCT/FR2009/000516 WO2009138598A2 (en) 2008-05-06 2009-04-30 Method and device for implementing the thrust reversers of an aircraft

Publications (1)

Publication Number Publication Date
BRPI0908328A2 true BRPI0908328A2 (en) 2016-07-05

Family

ID=40011094

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908328A BRPI0908328A2 (en) 2008-05-06 2009-04-30 propulsion inverters, control device and aircraft application process

Country Status (9)

Country Link
US (1) US8733698B2 (en)
EP (1) EP2297438B1 (en)
JP (1) JP5480888B2 (en)
CN (1) CN102105666B (en)
BR (1) BRPI0908328A2 (en)
CA (1) CA2721378C (en)
FR (1) FR2930973B1 (en)
RU (1) RU2449153C1 (en)
WO (1) WO2009138598A2 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2933072B1 (en) * 2008-06-30 2010-08-20 Airbus France METHOD AND DEVICE FOR DETECTION OF AN AIRCRAFT PUSHING DISSYMETRY TO BRAKE.
FR2958978B1 (en) * 2010-04-20 2014-04-18 Aircelle Sa ARRANGEMENT OF RODS OF PUSH REVERSING SHUTTERS ON THE FIXED INTERNAL STRUCTURE OF A TURBOREACTOR NACELLE
FR2992685B1 (en) * 2012-07-02 2016-05-27 Aircelle Sa METHOD FOR CONTROLLING A VARIABLE PIPE SECTION OF AN AIRCRAFT
CN102787994B (en) * 2012-08-25 2014-06-11 冯益安 Jet reducing power machine of jet automobile
FR2999656B1 (en) * 2012-12-17 2017-11-17 Snecma OPTIMIZING THE AVAILABILITY OF A PUSH INVERTER
US9650994B2 (en) * 2014-07-30 2017-05-16 The Boeing Company Thrust reverser actuator systems
US10443540B2 (en) * 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10497271B2 (en) * 2016-12-12 2019-12-03 The Boeing Company Runway exiting systems and methods for aircraft
FR3064602B1 (en) * 2017-03-29 2019-06-07 Airbus Operations DEGRADE OPERATING MODE OF AN AIRCRAFT PROPELLER GROUP FOR DEPLACING A PUSHING DIRECTION
US10119495B1 (en) * 2017-06-28 2018-11-06 General Electric Company System and method of operating a ducted fan propulsion system inflight
US10343786B2 (en) * 2017-06-28 2019-07-09 General Electric Company System and method of operating a ducted fan propulsion system during aircraft taxi
US10703498B2 (en) * 2017-11-02 2020-07-07 The Boeing Company Methods and aircraft for optimized reverse thrust operation during landing
FR3092819A1 (en) * 2019-02-18 2020-08-21 Airbus Operations TURBOREACTOR NACELLE CONTAINING A LOCKING DOOR AND A LOCKING DOOR DEPLOYMENT SYSTEM
FR3093993B1 (en) * 2019-03-21 2021-02-26 Safran Aircraft Engines A method of controlling the braking of the wheels of an airplane and the associated wheel braking controller
US11414175B2 (en) 2019-04-01 2022-08-16 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
US20200370510A1 (en) * 2019-05-21 2020-11-26 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
RU2719778C1 (en) * 2019-09-05 2020-04-23 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Control method of aircraft engine reversing device at aircraft braking
FR3105804B1 (en) * 2019-12-30 2021-12-03 Safran Nacelles Control system of a thrust reverser means of an aircraft
CN111679691A (en) * 2020-07-16 2020-09-18 深圳市澳玛禾经贸有限公司 Obstacle avoidance control system and method for aircraft and aircraft

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3168880A (en) * 1962-09-25 1965-02-09 Singer Co Stands for sewing machine cabinets
US3618880A (en) * 1970-05-11 1971-11-09 Boeing Co Speed brake system for aircraft spoilers
DE2354747A1 (en) * 1973-11-02 1975-05-07 Motoren Turbinen Union DEVICE FOR CONTROLLING A THRUST REVERSER
FR2580034B1 (en) * 1985-04-03 1987-05-29 Aerospatiale
GB9015373D0 (en) * 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
US5259187A (en) * 1993-02-05 1993-11-09 General Electric Company Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes
GB9418476D0 (en) * 1994-09-14 1994-11-02 Dunlop Ltd Sequential selective operation of aircraft brakes
FR2749041B1 (en) * 1996-05-23 1998-06-26 Hispano Suiza Sa DOUBLE FLOW TURBOREACTOR DRIVE INVERTER WITH PRIMARY HOOD OBSTACLES
FR2755730B1 (en) * 1996-11-14 1999-01-08 Hispano Suiza Sa ELECTRICAL CONTROL SYSTEM FOR A TURBOREACTOR DRIVE INVERTER
FR2846375B1 (en) * 2002-10-25 2006-06-30 Hispano Suiza Sa ELECTROMACANIC PUSH INVERTER FOR TURBOREACTOR WITH RELEASE OF DOOR MOVEMENT
FR2846376B1 (en) * 2002-10-25 2005-01-28 Hispano Suiza Sa MAINTENANCE AND INHIBITION PLATINUM FOR THRUST INVERTER
FR2859176B1 (en) * 2003-09-03 2005-10-28 Airbus France AIRCRAFT PROVIDED WITH PUSH REVERSERS
FR2872223B1 (en) * 2004-06-29 2006-08-25 Hurel Hispano Sa CONTROL METHOD FOR ACTUATING A THRUST INVERTER
US9043050B2 (en) * 2008-08-13 2015-05-26 The Boeing Company Programmable reverse thrust detent system and method

Also Published As

Publication number Publication date
US8733698B2 (en) 2014-05-27
CA2721378A1 (en) 2009-11-19
WO2009138598A2 (en) 2009-11-19
CN102105666A (en) 2011-06-22
US20110108665A1 (en) 2011-05-12
WO2009138598A3 (en) 2010-01-07
CN102105666B (en) 2013-10-02
EP2297438A2 (en) 2011-03-23
CA2721378C (en) 2015-09-29
FR2930973B1 (en) 2010-04-23
JP5480888B2 (en) 2014-04-23
EP2297438B1 (en) 2014-07-16
JP2011519776A (en) 2011-07-14
RU2449153C1 (en) 2012-04-27
FR2930973A1 (en) 2009-11-13

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]